A hybrid tube, in particular for an aircraft seat structure includes ribs intended to receive the hybrid tube. The hybrid tube includes a monolithic carbon tube and at least one sleeve made from a ductile material and connected to the carbon tube by means of gluing, shrink-fitting or over-molding.
TUBE DE STRUCTURE DE TYPE HYBRIDE, NOTAMMENT POUR SIÈGE AÉRONAUTIQUE
TUBE HAVING A HYBRID-TYPE STRUCTURE, IN PARTICULAR FOR AN AIRCRAFT SEAT
ROHR MIT EINER HYBRIDARTIGEN STRUKTUR, INSBESONDERE FÜR EINEN FLUGZEUGSITZ
28.04.2021
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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